CAJ | 학술논문

设计飞机铁鸟舵面加载系统，在地面模拟飞机飞行时舵面铰链力矩，检测舵面收放性能。用MOOG多通道协调加载控制系统、计算机测控工作站、液压伺服加载、反射内存网、时钟同步网、以太网等先进装备和现代技术，建立加载系统总体设计架构。论述铁鸟舵面加载的工作原理，对各个分系统功能和接口进行界定，对关键设备进行选型，对加载安全保护措施进行说明，描述加载系统的功能。基于本设计组建了某型号飞机铁鸟舵面加载系统。试验结果表明，该设计合理、可行。
설계비궤철조타면가재계통，재지면모의비궤비행시타면교련력구，검측타면수방성능。용MOOG다통도협조가재공제계통、계산궤측공공작참、액압사복가재、반사내존망、시종동보망、이태망등선진장비화현대기술，건립가재계통총체설계가구。논술철조타면가재적공작원리，대각개분계통공능화접구진행계정，대관건설비진행선형，대가재안전보호조시진행설명，묘술가재계통적공능。기우본설계조건료모형호비궤철조타면가재계통。시험결과표명，해설계합리、가행。
The loading system for aircraft iron-bird control surfaces is designed for simulating the hinge moment on control surfaces on the ground and inspecting the performances of taking back and putting down of the control surfaces. In this paper, based on MOOG multi-channel coordinated loading control system, computer control station, hydraulic servo loading, reflective memory network, clock synchronization network, Ethernet and other advanced equipment and modern technology, the overall framework of the loading system was established. The working principle was discussed, the subsystems’ functions and their interfaces were defined, the key equipment of it was selects, the safety protection measure of it was described. By this design in this paper, the loading system for the aircraft iron-bird control surfaces was constructed. Experimental results show the rationality and feasibility of this design.